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1.
三点弯曲试样动态冲击特性的有限元分析   总被引:6,自引:0,他引:6  
本文使用动态有限元技术,对两种不同几何尺寸,两种不同材料的三点弯曲试样在三类七种不同冲击载荷作用下的动态响应进行了分析,求得了动态应力强度因子随时间的变化规律,并与准静态应力强度因子进行了比较,计算结果表明:半冲击载荷历史代入静态公式确定动态应力强度因子的做法是不正确的,要求得动态应力强度因子,必须对试样进行完全的动态分析,当材料的E/ρ值相同时,动态应力强度因子的响应曲线完全相同,而动态应力强度  相似文献   

2.
本文使用动态有限元技术,对于两种不同几何尺寸,两种不同材料的三点弯曲试样在三类七种不同冲击载荷作用下的动态响应进行了分析,求得了动态应力强度因子随时间的变化规律。并与准静态应力强度因子进行了比较。计算结果表明:将冲击载荷历史代入静态公式确定动态应力强度因子的做法是不正确的,要求得动态应力强度因子,必须对试样进行完全的动态分析。当材料的E/ρ值相同时,动态应力强度因子的响应曲线完全相同。而动态应力强度因子分别与加载点的位移及裂纹的张开位移之间存在着与准静态情况下各自相同的线性关系。这与资料[5][6]中的结论完全相同。  相似文献   

3.
高加载率下Ⅱ型裂纹试样的动态应力强度因子及断裂行为   总被引:4,自引:1,他引:3  
采用Hopkinson单压杆技术对单边平行双裂缝试样进行高速剪切加载,用实测的试样加载面上的载荷p(t)结合有限元计算确定其动态应力强度因子。同时还发展了一种用实测的裂尖动态应变,通过在准静态下标定的裂尖应变与应力强度因子间的关系来确定动态应力强度因子的近似方法。实验结果表明,对于稳定裂纹在无边界反射应力波干扰的情况下,两种方法获得的动态应力强度因子吻合得相当好。对40Cr钢和Ti6Al4V钛合金两种材料的动态Ⅱ型断裂实验结果显示出两种完全不同的剪切破坏模式和机理。  相似文献   

4.
用裂纹张开位移计算三点弯曲试样的动态应力强度因子   总被引:4,自引:0,他引:4  
给出了一种由裂纹的动态张开位移计算三点弯曲试样的动态应力强度因子的简单方法。对于两种不同几何尺寸的试样,在三类不同载荷作用下给出了数植算例,并与完全的动态有限元方法的计算结果进行了比较。结果表明:两种方法的计算结果相当一致。最后,还给出了由测定三点弯曲试样的裂纹张开位移确定试样的动态应力强度因子,最终确定材料动态起裂韧性的方法。  相似文献   

5.
三点弯曲试样动态应力强度因子计算研究   总被引:2,自引:0,他引:2  
利用Hopkinson压杆对三点弯曲试样进行冲击加载,采集了垂直裂纹面距裂尖2mm和与裂纹面成60°距裂尖5mm处的应变信号。根据裂尖附近测试的应变信号计算试样的动态应力强度因子,并与有限元计算结果进行比较,结果表明由于裂尖有一段疲劳裂纹区,通过裂尖附近应变信号来计算动态应力强度因子时,如果裂尖位置确定不准及粘贴应变片位置不够准确对计算结果将带来很大影响。因此利用应变片法计算动态应力强度因子时,为了获得更准确的计算结果,在实验后应对试件裂纹面进行分析测量,重新确定裂尖位置,必要时需对应变片至裂尖距离进行修正后再计算动态应力强度因子值。  相似文献   

6.
三点弯曲试样应力强度的动态响应   总被引:1,自引:0,他引:1  
采用振动理论分析了三点弯曲试样的动态响应,得到了一个计及冲击速度影响的动态应力强度因子计算公式。当不考虑冲击速度影响时,本文给出的计算模型可退化成经典的K.Kishimoto模型。数值计算的结果表明,无论是在阶跃载荷作用下,还是在周期载荷作用下,冲击速度对三点弯曲试样应力强度因子的动态响应都有明显的影响。  相似文献   

7.
40Cr材料动态起裂韧性KId()的实验测试   总被引:4,自引:0,他引:4  
描述了利用Hopkinson压杆技术加载三点弯曲试样测试40Cr,材料动态起裂韧性KId()的试验方法。试样上的动态载荷历程由Hopkinson杆直接测得,并分别代入动态有限元程序及近似公式求得动态应力强度因子历史;由贴在试样裂尖附近的应变片确定起裂时间,最终确定起裂时的动态应力强度因子值,即动态起裂韧性KId()。试验结果表明:利用Hopkinson压杆技术加载三点弯曲试样测试材料动态起裂韧性的方法是可行的,起裂时,动态有限元的位移法、应力法及近似公式法求得的动态应力强度因子值比较吻合;在本文的载荷速率下,40Cr材料动态起裂韧性KId()与准静态裂韧性KId()相比,降低了约28%。  相似文献   

8.
高应变率下断裂韧性实验的数值模拟   总被引:1,自引:0,他引:1  
采用有限元软件ANSYS/LS-DYNA程序对静态和冲击荷载作用下的含裂纹半圆弯曲(SCB)实验进行了数值模拟。根据静态实验的模拟结果,提出了适合复合型加载的Ⅰ型应力强度因子拟合公式,采用该公式计算应力强度因子的最大误差不超过10%。动态实验的模拟结果表明:对于纯Ⅰ型加载的SCB实验,动态应力强度因子随着试样半径、支座间距以及相对裂纹长度的变化呈现规律性变化;当试样半径小于60mm、相对支座间距为1.2、相对裂纹长度在0.1~0.4范围内时,惯性效应的影响较小,采用静态拟合公式计算裂尖的动态应力强度因子的误差约10%;对于复合型加载的SCB实验,当相对裂纹长度为0.2~0.4、裂纹倾角在10°~40°范围内时,采用静态拟合公式计算裂尖的动态应力强度因子的误差小于10%。  相似文献   

9.
材料的动态断裂韧性是衡量材料在动载荷作用下抵杭裂纹扩展能力的重要指标,以往的材料动态断裂韧性测试多采用三点弯曲试样,而针对紧凑拉伸试样的动态断裂韧性研究很少.本文将紧凑拉伸试样(即CT试样)简化成等效弹簧质量模型,得到了CT试样动态应力强度因子的近似表达式.对Hopkinson压杆装置进行了改进,利用改进后的实验装置进...  相似文献   

10.
中心直裂纹平台巴西圆盘复合型动态应力强度因子   总被引:2,自引:0,他引:2  
为了指导用中心直裂纹平台巴西圆盘(CSTFBD)试样进行岩石复合型动态断裂 试验,利用有限元法首先验证了文献中对中心直裂纹巴西圆盘(CSTBD)得到的有关结果,分析 比较了不同无量纲裂纹长度(即裂纹半长和圆盘半径之比)时两种圆盘的I, II型动态应力 强度因子的时间历程,发现两者的差异大部分在10{\%}以内,同时验证了该文数值方法的可 靠性. 然后讨论了CSTFBD试样I, II型动态应力强度因子的复合比、起裂角以及纯II型加 载角. 研究成果可为复合型动态断裂试验中CSTFBD试样的加工、试样上应变片的粘贴、起裂 方向和起裂时间的估计等提供参考.  相似文献   

11.
By using the well-developed integral transform methodology, the dynamic response of stress and electric displacement around a finite crack in an infinite piezoelectric strip are investigated under arbitrary dynamic anti-plane loads. The dynamic stress intensity factors and electric displacement are obtained analytically. It is shown that the dynamic crack-tip stress and electric field still have a square-root singularity. Numerical computations for the dynamic stress intensity factor show that the electric load has a significant influence on the dynamic response of stress field. The higher the ratio of the crack length to the width of the strip, the higher the peak value of the dynamic stress intensity factor is. On the other hand, the dynamic response of the electric field is determined solely by the applied electric load. The electric field will promote or retard the propagation of the crack depending on the time elapse since the application of the external electro-mechanical loads. The project supported by the National Natural Science Foundation of China and the Post-Doctor Science Foundation of China  相似文献   

12.
IntroductionInrecentyears,greatattentionshavebeenpaidtotheresearchofFunctionallyGradedMaterials(FGM).Fromtheviewpointsofappliedmechanics,FGMarenon_homogeneoussolids.Thenon_homogeneityofFGMhasagreatinfluenceontheirmechanicalbehavior,especiallywhenthecomp…  相似文献   

13.
A dynamic weight function method is presented for dynamic stress intensity factors of circular disk with a radial edge crack under external impulsive pressure. The dynamic stresses in a circular disk are solved under abrupt step external pressure using the eigenfunction method. The solution consists of a quasi-static solution satisfying inhomogeneous boundary conditions and a dynamic solution satisfying homogeneous boundary conditions. By making use of Fourier-Bessel series expansion, the history and distribution of dynamic stresses in the circular disk are derived. Furthermore, the equation for stress intensity factors under uniform pressure is used as the reference case, the weight function equation for the circular disk containing an edge crack is worked out, and the dynamic stress intensity factor equation for the circular disk containing a radial edge crack can be given. The results indicate that the stress intensity factors under sudden step external pressure vary periodically with time, and the ratio of the maximum value of dynamic stress intensity factors to the corresponding static value is about 2.0.  相似文献   

14.
Three-dimensional elliptic crack under impact loading   总被引:4,自引:0,他引:4  
The dynamic stress intensity factor of a three-dimensional elliptic crack under impact loading is determined with the finite element method. The computation results can take into account the influence of time and the ratio of the wave speeds on the stress intensity factor. The present method is suitable not only for three-dimensional dynamic crack, but also for three-dimensional dynamic contact. Project supported by the National Natural Science Foundation of China (No. K19672007).  相似文献   

15.
A mathematical formulation is presented for the dynamic stress intensity factor (mode I) of a finite permeable crack subjected to a time-harmonic propagating longitudi-nal wave in an infinite poroelastic solid. In particular, the effect of the wave-induced fluid flow due to the presence of a liquid-saturated crack on the dynamic stress intensity fac-tor is analyzed. Fourier sine and cosine integral transforms in conjunction with Helmholtz potential theory are used to formulate the mixed boundary-value problem as dual inte-gral equations in the frequency domain. The dual integral equations are reduced to a Fredholm integral equation of the second kind. It is found that the stress intensity factor mono-tonically decreases with increasing frequency, decreasing the fastest when the crack width and the slow wave wavelength are of the same order. The characteristic frequency at which the stress intensity factor decays the fastest shifts to higher frequency values when the crack width decreases.  相似文献   

16.
功能梯度材料裂纹尖端动态应力场   总被引:10,自引:2,他引:8  
研究受反平面剪切作用的功能梯度材料动态裂纹问题,通过积分变换-对偶积分方程方法推出了裂纹尖端动态应力场,时间域内的动态应力强度因子由Laplace数值反演获得,研究结果表明功能梯度材料的梯度越大,相应的裂纹问题的动态应力强度因子值越低。  相似文献   

17.
This paper analyzes the dynamic magnetoelectroelastic behavior induced by a penny- shaped crack in a magnetoelectroelastic layer.The crack surfaces are subjected to only radial shear impact loading.The Laplace and Hankel transform techniques are employed to reduce the prob- lem to solving a Fredholm integral equation.The dynamic stress intensity factor is obtained and numerically calculated for different layer heights.And the corresponding static solution is given by simple analysis.It is seen that the dynamic stress intensity factor for cracks in a magnetoelec- troelastic layer has the same expression as that in a purely elastic material.And the influences of layer height on both the dynamic and static stress intensity factors are insignificant as h/a>2.  相似文献   

18.
The method of complex function and the method of Green‘s function are used to investigate the problem of SH-wave scattering by radial cracks of any limited length along the radius originating at the boundary of an elliptical hole, and the solution of dynamicstress intensity factor at the crack tip was given. A Green‘s function was constructed for the problem, which is a basic solution of displacement field for an elastic half space containing a half elliptical gap impacted by anti-plane harmonic linear source force at any point of its horizontal boundary. With division of a crack technique, a series of integral equations can be established on the conditions of continuity and the solution of dynamic stress intensity factor can be obtained. The influence of an elliptical hole on the dynamic stress intensity factor at the crack tip was discussed.  相似文献   

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